View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 11672U 80005B 23341.49485994 .00000596 00000-0 60584-4 0 9992
2 11672 82.5157 6.9431 0016914 30.8653 329.3556 14.89028047353902
| Epoch (UTC): | 07 December 2023 11:52:35 |
| Eccentricity: | 0.0016914 |
| inclination: | 82.5157° |
| perigee height: | 589 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 6.9431° |
| argument of perigee: | 30.8653° |
| revolutions per day: | 14.89028047 |
| mean anomaly at epoch: | 329.3556° |
| orbit number at epoch: | 35390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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